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CA1082456A - Apparatus for refining molten metal - Google Patents

  • ️Tue Jul 29 1980

CA1082456A - Apparatus for refining molten metal - Google Patents

Apparatus for refining molten metal

Info

Publication number
CA1082456A
CA1082456A CA284,080A CA284080A CA1082456A CA 1082456 A CA1082456 A CA 1082456A CA 284080 A CA284080 A CA 284080A CA 1082456 A CA1082456 A CA 1082456A Authority
CA
Canada
Prior art keywords
vessel
apparatus defined
melt
blocks
lining
Prior art date
1976-08-16
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA284,080A
Other languages
French (fr)
Inventor
Andrew G. Szekely
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Union Carbide Corp
Original Assignee
Union Carbide Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
1976-08-16
Filing date
1977-08-04
Publication date
1980-07-29
1977-08-04 Application filed by Union Carbide Corp filed Critical Union Carbide Corp
1980-07-29 Application granted granted Critical
1980-07-29 Publication of CA1082456A publication Critical patent/CA1082456A/en
Status Expired legal-status Critical Current

Links

  • 229910052751 metal Inorganic materials 0.000 title claims abstract description 34
  • 239000002184 metal Substances 0.000 title claims abstract description 34
  • 238000007670 refining Methods 0.000 title claims abstract description 13
  • 238000010438 heat treatment Methods 0.000 claims abstract description 30
  • 239000000155 melt Substances 0.000 claims abstract description 30
  • OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 17
  • 229910002804 graphite Inorganic materials 0.000 claims abstract description 17
  • 239000010439 graphite Substances 0.000 claims abstract description 17
  • HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims abstract description 8
  • 229910010271 silicon carbide Inorganic materials 0.000 claims abstract description 8
  • 239000007789 gas Substances 0.000 claims description 27
  • 230000008602 contraction Effects 0.000 claims description 2
  • 238000007654 immersion Methods 0.000 description 8
  • 230000009977 dual effect Effects 0.000 description 6
  • 239000000463 material Substances 0.000 description 6
  • 230000001681 protective effect Effects 0.000 description 6
  • 238000005266 casting Methods 0.000 description 5
  • 230000003628 erosive effect Effects 0.000 description 5
  • 229910001018 Cast iron Inorganic materials 0.000 description 4
  • 229910045601 alloy Inorganic materials 0.000 description 4
  • 239000000956 alloy Substances 0.000 description 4
  • 239000011449 brick Substances 0.000 description 4
  • 229910000831 Steel Inorganic materials 0.000 description 3
  • 230000007797 corrosion Effects 0.000 description 3
  • 238000005260 corrosion Methods 0.000 description 3
  • 239000006185 dispersion Substances 0.000 description 3
  • 239000012535 impurity Substances 0.000 description 3
  • 239000011261 inert gas Substances 0.000 description 3
  • 238000009413 insulation Methods 0.000 description 3
  • 239000010959 steel Substances 0.000 description 3
  • XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
  • UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
  • XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
  • 229910018487 Ni—Cr Inorganic materials 0.000 description 2
  • 229940037003 alum Drugs 0.000 description 2
  • 229910052782 aluminium Inorganic materials 0.000 description 2
  • XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
  • VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 0.000 description 2
  • 238000010586 diagram Methods 0.000 description 2
  • 238000005485 electric heating Methods 0.000 description 2
  • 239000001257 hydrogen Substances 0.000 description 2
  • 229910052739 hydrogen Inorganic materials 0.000 description 2
  • 239000012212 insulator Substances 0.000 description 2
  • 238000000034 method Methods 0.000 description 2
  • RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
  • ZAKOWWREFLAJOT-CEFNRUSXSA-N D-alpha-tocopherylacetate Chemical compound CC(=O)OC1=C(C)C(C)=C2O[C@@](CCC[C@H](C)CCC[C@H](C)CCCC(C)C)(C)CCC2=C1C ZAKOWWREFLAJOT-CEFNRUSXSA-N 0.000 description 1
  • FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
  • ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
  • HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
  • YKTSYUJCYHOUJP-UHFFFAOYSA-N [O--].[Al+3].[Al+3].[O-][Si]([O-])([O-])[O-] Chemical compound [O--].[Al+3].[Al+3].[O-][Si]([O-])([O-])[O-] YKTSYUJCYHOUJP-UHFFFAOYSA-N 0.000 description 1
  • PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
  • 229910052786 argon Inorganic materials 0.000 description 1
  • 230000015572 biosynthetic process Effects 0.000 description 1
  • 229910052802 copper Inorganic materials 0.000 description 1
  • 239000010949 copper Substances 0.000 description 1
  • 230000007812 deficiency Effects 0.000 description 1
  • 238000003795 desorption Methods 0.000 description 1
  • 238000001914 filtration Methods 0.000 description 1
  • 238000007667 floating Methods 0.000 description 1
  • 238000005188 flotation Methods 0.000 description 1
  • 239000011888 foil Substances 0.000 description 1
  • 239000000446 fuel Substances 0.000 description 1
  • 239000007770 graphite material Substances 0.000 description 1
  • 238000002347 injection Methods 0.000 description 1
  • 239000007924 injection Substances 0.000 description 1
  • 238000003780 insertion Methods 0.000 description 1
  • 230000037431 insertion Effects 0.000 description 1
  • 238000009434 installation Methods 0.000 description 1
  • 229910052742 iron Inorganic materials 0.000 description 1
  • 239000011133 lead Substances 0.000 description 1
  • 229910052749 magnesium Inorganic materials 0.000 description 1
  • 239000011777 magnesium Substances 0.000 description 1
  • 239000013528 metallic particle Substances 0.000 description 1
  • 150000002739 metals Chemical class 0.000 description 1
  • 239000000203 mixture Substances 0.000 description 1
  • 230000003647 oxidation Effects 0.000 description 1
  • 238000007254 oxidation reaction Methods 0.000 description 1
  • 239000003973 paint Substances 0.000 description 1
  • 239000002245 particle Substances 0.000 description 1
  • 230000002829 reductive effect Effects 0.000 description 1
  • 239000011819 refractory material Substances 0.000 description 1
  • 230000000452 restraining effect Effects 0.000 description 1
  • 230000000717 retained effect Effects 0.000 description 1
  • 238000007789 sealing Methods 0.000 description 1
  • 229910052710 silicon Inorganic materials 0.000 description 1
  • 239000010703 silicon Substances 0.000 description 1
  • 238000004513 sizing Methods 0.000 description 1
  • 125000006850 spacer group Chemical group 0.000 description 1
  • 239000000725 suspension Substances 0.000 description 1
  • 229910052718 tin Inorganic materials 0.000 description 1
  • 239000011135 tin Substances 0.000 description 1
  • 238000009736 wetting Methods 0.000 description 1
  • 229910052725 zinc Inorganic materials 0.000 description 1
  • 239000011701 zinc Substances 0.000 description 1
  • NWONKYPBYAMBJT-UHFFFAOYSA-L zinc sulfate Chemical compound [Zn+2].[O-]S([O-])(=O)=O NWONKYPBYAMBJT-UHFFFAOYSA-L 0.000 description 1

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27DDETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D27/00Stirring devices for molten material
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22BPRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
    • C22B21/00Obtaining aluminium
    • C22B21/06Obtaining aluminium refining
    • C22B21/064Obtaining aluminium refining using inert or reactive gases
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22BPRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
    • C22B9/00General processes of refining or remelting of metals; Apparatus for electroslag or arc remelting of metals
    • C22B9/05Refining by treating with gases, e.g. gas flushing also refining by means of a material generating gas in situ
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27BFURNACES, KILNS, OVENS OR RETORTS IN GENERAL; OPEN SINTERING OR LIKE APPARATUS
    • F27B14/00Crucible or pot furnaces
    • F27B14/06Crucible or pot furnaces heated electrically, e.g. induction crucible furnaces with or without any other source of heat

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Manufacturing & Machinery (AREA)
  • General Engineering & Computer Science (AREA)
  • Vertical, Hearth, Or Arc Furnaces (AREA)
  • Treatment Of Steel In Its Molten State (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Furnace Details (AREA)
  • Casting Support Devices, Ladles, And Melt Control Thereby (AREA)

Abstract

APPARATUS FOR REFINING MOLTEN METAL

ABSTRACT OF THE DISCLOSURE

A vessel adapted for maintaining metal in a molten state comprising, in combination:
(a) an insulating refractory shell impervious to molten metal;
(b) a lining for a major proportion of that interior surface of said shell, which will be below the surface of the melt, said lining comprising graphite or silicon carbide blocks, which are free to expand in at least one direction in response to the application of heat; and (c) at least one heating means disposed within any of the blocks.

S P E C I F I C A T I O N

Description

10~2~5f~

FIELD OF THE INVENTION

This invention relates to apparatus used in metal refining, particularly that associated with refining molten metal. ~`

Description of the Prior Art Although the invention described herein has general application in refining molten metals, it is particularly relevant in refining aluminum, magnesium, copper, zinc, tin, lead, and their alloys and is considered to be an improvement over the apparatus described in United States patent number 3,870,511 issued March 11, 1975.
Basically, the process carried out in the reference apparatus involves the dispersion of a sparging gas in the form of extremely small gas bubbles throughout a melt. Hydrogen is removed fro~ the melt by desorption in~ the gas bubbles, while other non-metallic impurities are lifted into a dross layer by flotation. The dispersion of the sparging gas is accomplished by the use of rotating gas distributors, which throw the melt into a highly turbulent state. m e turbulence causes the small non-metallic particles to agglomerate into large particle aggregates which are floated to the melt surface by the gas bubbles. This turbulence in the ,.

o, 971 .
~08Z~S~ i metal also assures thorough mixing of the sparging gas with the melt and keeps the interior of the vessel free from deposits and oxide buildups. Non-metallic impurities floated out of the metal are withdrawn from the system with the dross while the hydrogen desorbed from the metal leaves the system with the spent sparging gas~
The furnace presently used in the commercial application of the process comprises an external heating shell containing electrical heating elements and an inner cast iron shell lined with graphite and silicon carbide plates. Although this furnace apparatus has proved to be satisfactory, $t is found to have limitations ln certain applications.
One limitation invol~es the service life of the inner cast iron shell, which must be replaced at regular intervsls thus creating a dependence on a foundry.
It will be understood that it would be more advantageous if an insulating refractory, one that is castable or of cemented bricks, for exa~ple, which has a longer life and is easily repairable, could be used in the place of the cast iron shell, but this i6 only practical if the erosion inherent in the refractory with the accompanying generation of impurities can be countered. Another limitation is involved with an element of design, i.e., the provision of tap or drain holes for the melt, a lo, 97 108Z45~;

requirement of many furnaces where frequent alloy changes are made. The problem arises in that the provision of tap holes for externally heated furnaces is technically unfeas~ble. Still another limitation is that of providing metal inlet and outlet ports a~ different locations in the furnace for different customers. In the cast iron ~hell, the location of these ports is fixed by the casting pattern used by the foundry for casting the iron shell.
Changes in the casting pattern are uneconomic because 80 many different patterns are required. In contrast, the refractory shell can be custom built to meet customer needs.
In order to use an insulating refractory shell, however, external heating means can no longer be used, but, rather, some form of internal heating is needed.
The use of immersion heating has been suggested, but suffers from serious liabilities, e.g., the introduction of immersion heaters interferes with the bubble pattern in cases where the metal is sparged with a gas. It also interferes with the free movement or physical state of the melt, particu}arly the flow of the metal through filter media or ~he furnace. The use of immersion heaters ~8 also less than satisfactory ~n an alum~num filtering system since the insertion of the heaters ~n the filtrat~on medium has to be accommodated initially ~nd on replac~ment.

lo, 97 1~8~456 A further deficiency in typical immersion heaters is that they canno~ withstand an environment of high turbulence for any length of time. This stems from the fact that the heating device of the immersion heater needs a protective shell, which has a high thermal conductivity, is capable of withstanding high temperatures, and is inert to the melt an~ corrosion resistant. These protective shells are usually thin walled to provide good thermal conduction and for economic reasons, however, they have a relatively short life under exposure to high turbulence. The problem is further aggravated by the manner in which the immersion heaters are su~pended in the melt, the suspension by its very nature providing very little support against the forces of ag~tation to which the immersion heater is exposed.

Summary of the Invention An object of this invention, therefore, is to provide spparatus for metal refining which provides an internal heating 60urce while overcoming the drawbacks of the immersion heater, msximizes shell life, minimizes erosion, i8 easily repairable, and economically accepts tap ho~es and custom~zing insofar as metal ~n~et and outlet ports are concerned.
Other ob~ects and atvantages will become apparent hereinafter.

o, 97 ~082~S6 Accor~ing to the present invention, such apparatus has been discovered in the form of a vessel adapted for maintaining metal in a molten state comprising, in combination;
~ a) an insulating refractory shell impervious to molten metal;
(b) a lining for a ma~or proportion of that interior surface of said shell, which will be below the surface of the melt, sait lining comprising graphite or silicon carbide blocks, which are free to expand in at least one direction in response to t~e application of heat; and (c) at least one heating means disposed within any of the blocks.
The de~cribed ve~sel finds a preferret application in apparatus comprising, in combination:
(d) the ves~el defined above in (a), (b), and (c ) ;
(e) at least one rotating gas distributing means disposed in ~aid ves~el, and (f) inlet and outlet means for molten metal and gases~

Brief Description of the ~rawing ~igure 1 i8 a perspective view of a preferred embodiment of rotating gas distributing means as shown - lo, 97 ~0824S6 in US 3,870,511 referred to above.
Figure 2 is a schematic diagram of a plan view Qhowing a preferred embodiment of the apparatus including the defined vessel and single rotating gas distributing means.
F~gure 3 is a schemat~c diagram in cross-sect~on taken along 3-3 of the embodiment shown in Figure 2.

Description of the Preferred Embod~ment The entire structure utilized in melt refining may be referred to as a furnace and is generally comprised of an outer steel shell lined first with an insulating ~-refractory such as brick cemented with, e.g., an alumina-~ilica mixture. Ihe first insulat~ng liner is then linet with an impervious refractory liner, which is also an insulator and usually a castable alumina, but can also be cemented brick. Both the first and second refractory linings are made of conventional msterials having good insulating properties and of sufficient thickne~s to keep the heat losses from the furnace at econom~cally acceptable levels. Although the u~e of ; ~ the ~teel shell and first insulating refractory are - suggested, the present inv~ntion simply requires that an insulat~ng refractory shell impervious to molten metal h~ving a thermal conductivity lower than about 0.5 BTU/
s~uare foot/hour/~Flfoot be used. These refractories lo ,97 l~Z4S6 are usually cured prior to use.
This refractory shell is then lined with "blocks"
comprised of a high thermal conductivity material, which is inert to the melt and corrosion resistant, and whose ~urface repels or resists wetting by the melt. The thermal conductivity is at least about 5-BTU/square foot/
hour/F/foot.
The term '~locks" is defined herein to mean a ~ --prefabricated piece of material that has a specified form. Common forms of blocks are conventional, e.g., plates and blocks wh~ch are often in the form of rectangular -prisms, the difference between the plate and block usually being a matter of thickness. These blocks are equipped with holes, recesses, or the like needed for their installation or function. The blocks (as defined) are preferably graphite or silicon carbide blocks or both. A ma~or proportion or more than 50 percent of the interior surface of the shell is covered with these blocks. T~e interior surface with which we are concerned here i8 that which w~ll be below the level of the melt under operating conditions. ~referably, more than about 75 percent of the interlor surface i~ covered with these -~ bloc~s. In B rectangular prism-~hsped structure having one compartment usua}ly the bottom and at least three sides are covered. In such a structure having, e.g., a working compartment where there i8 turbulence snd an :

lo, 97 108Z4S~;

exit compartment where there is no turbulence,usually the bottom and at least two sides of the working compartment are covered snd a wall is used to separate the exit compartment from the working compartment, the exit compartment be~ng unlined or lined. It is understood that the separating wall is not considered to be part of the lining. Other characteristics of the blocks are (a) relatively low thermal expansion coefficients; (b) a ratio of thermal conductivity to the thermal expansion :-coefficient larger than 3.106 (room temperature values expressed in units of BTU/square foot/hour/F/foot and inch/inch/F, respectively); and (c) resistant to erosion by agitated molten metal.
It will be understood that the materials used for the interior surface or lining above the level of the melt is not critical here, but inert and corrosion resistant materials should at least be considered ~n view of the exposure to ~pray from the melt.
One function of the blocks is to protect the refractory shell against erosion caused by the melt and, jto th~s ~nd, the greater the interior surface that is ¦covered the better. Usually, the interior surface of the re~r~c~ory shell is only exposed ~ecau~e of de~ign limitations.
The ~locks are installed ~n such a manner that their thermal movement is unrestricted in at least one _g_ .. .

10,971 10~2~S6 d~rection and usually two directions. They may be attached to the interior surface of the shell or to each other at one point or another. The melt may penetrate between and behind the blocks, but is minimized as design -permits. Any restriction placed on the thermal expansion of the blocks is again due to overriding design limitations, e.g., to keep size to a minimum. The blocks are kept in place by some conventional restraining device or medium, e.g., the shell itself, slots or recesses into which the block can be slipped, or one block can restrain another.
The blocks are of varying thickness depending on their functlon in the furnace. Two kinds of blocks are utillzed here. The function of one kind of block is merely to protect the interior surface of the refractory from erosion. The thickness of this protective block is generally about 1 to about 5 inches. The second kind has a dual function, one, that of the protective block, and, the other function, that of housing an electric heating element or elements or flame heating ; devices. The thickness of the dual function block is generally about 3 to about 10 inches. The dual function block contains at least one heating device and usually several, e.g., 2 to 4, especially where it cover~ the inter~or surface of one of the walls of the furnace.
It should be noted that one or se~eral block~ can be u~ed o, 97 ~8.Z456 to cover a particular surface restrained as noted above.
A sufficient number of heating devices is provided to maintain the metal in the molten state. This number is related to the intensity of the heating device, e.g., the energy supplied by the flame or per one electric heating element; to the melt volume; and to the heat losses from the outside of the furnace. In applications where metal is flowing through the furnace and it i8 desired to increase the temperature of the molten metal, the metal flow rate and the intended heating rate define the total power input to the furnace, and in turn, the sizing of the heating devices and blocks. The number of heating devices may range from 1 to 6 or more.
In the ca~e of graphite, the heating device is an electric resistance heating element housed in 6uch a manner that it does not contact the plate. The heating device used in 6ilicon carbide plates, however, can be the same as for graphite or a flame heating device using conventional gas fuels.
The heating element can be a nickel-chromium element or any conventional resistance heating element which can provide temperatures sufficient to maintain the particular metal or alloy in the molten state, e.g., temperatures of about 1000F to about 2500F.
Referring to tbe drawing:
Figure 1 exemplifie~ preferred rotating gas distribut-lo, 97 1082~S6 ing means.l It can also be referred to as a gas inject~on device. The device is comprised of rotor 1 equipped with vertical vanes 2. The rotor is rotated by means of a motor (not shown) through shaft 3. Shaft 3 is shielded from the melt by sleeve 4 which is f~xedly attached to stator 5. The internal design of the device is such that gas can be introduced into the interior of the device and forced out between stator 5 and rotor 1. The stator has channels 6, w~ich correspond to vanes 2 of the rotor.
The Bimultaneous g8S injection and rotor rotation at sufficient pressure and rotation speed cause the desired dispersion pattern of sparging gas in melt creating an env~ronment of high turbulence. Specifics of the device and the circulation pattern may be obtained from US
3,870,511.
The apparatus ~hown in Figures 2 and 3 has a single rotating gas distributing means 1 which is similar to the device shown in Flgure 1. Outer wall 2 of the furnace ~s typically made of steel. Ins~de of wall 2 is refractory 3 of low thermal conductivity cemented brick as a first insulator and inside refractory 3 is ¦ refractory 4, a castable alumins impervious to the melt.
A typ~cal castable alum~na ~8 96% A12o3, 0.2% Fe203, and balance other materials. ~efractory 4 i9 also of low thermal conducti~ity and, of course, provides further insulation. The outer structure i6 completed with lo ,97 iO82~S6 furnace cover or roof 5 and a superstructure (not shown), which supports gas distributor 1 and an electric motor (not shown).
Since the preferred embodiment uses graphite materials extensively and is intended for a high purity refining operation, it will be understood that the system is adequately sealed and protected by a blanket of inert gas to provide an essentially air-free environment.
Where the vessel is 80 sealed, it will be referred as a "closed" vessel. There are metal refining operations and other instances, e.g., a melt holding situation, where such an environment is not required. Silicon ;-carbide can, of course, be uset in both cases. In the latter case, however, air-tight seals and a protective covering of inert gas can be dispensed with. It is contemplated that the ve~sel proposed here be used in either type of operation and any structure of the described apparatus outside of the defined vessel which is not of value in the latter operation can be omitted for econ ic reaso~s or otherwise as the operator sees fit.
The refining operation begins with the opening of sliding doors (not shown) at the entrance of inlet port 7. The molten metal enters working compartment ~ (ghown with melt) through inlet port 7 which may be lined with silicon carbide blocks. The melt is vigorously stirred and ~parged with refining gas through rotating gas lo ,97 108Z4~;

di6tributor 1. The rotation of the rotor of tistributor 1 is counterclockwise, ~owever, the circulation pattern induced ~n the melt by distributor 1 has a vertical component. Vortex formation is reduced by offsetting the symmetry of work~ng compartment 8 w~th exit pipe 9 and baffles 10 and 15.
The refined metal enters exit pipe 9 located behind baffle 10 and is conducted into exit compartment 11.
Compartment 11 is separated from working compartment 8 by graphite block 12 and silicon carbide block 13. The refined metal leaves the furnace through exit port 14 and is conducted, for example, to a casting machine under a level flow. The bottom of the furnace is lined with graphite plate 6.
The dross floating on the metal is caught by block 15 acting as bot~ a baffle and a skimmer and collects on the ~urface of the melt close to inlet port 7 from where it can easily be removed. The spent sparging gas leaves the system beneath the ~liding doors (not shown)

2~ at the entrance. Head space protect~on over the melt ~ is provided ~y introduclng an inert gas such as argon into ¦ the furnace through an inlet pipe (not ~hown). The atmosphere in exit compartment 11, however, iB not controlled and, therefore, graphite bloc~ 12 is used there only ~elow the surface of the melt.
A feature of this invention is the avoidance of lo, 97 turbulence in exit c~mpartment 11, i.e. the melt in that section is in an almost quiescent state, which is advantageous in providing a level flow to casting. This is achieved by exit pipe 9 which dampens the turbulence.
Tap or drain hole 16 is provided for draining the furnace when alloy changes are made. It can be located on the inlet or outlet side of the furnace.
Heat is supplied to the furnace, in this embodiment, by 8ix nickel-chromium electric resistance heating elements 17 which are in~erted into dual function graphite blocks 18, three in each block. Blocks 18 are kept in -place by steel clips 19 and by blocks 12 and 13, which, in turn, are retained by the use of slots and recesses (not shown). Blocks 18 are free to expand toward the inlet 8ide of the furnace and upward.
~oof 5 is in a sealed relationship with the rest of the furnace through the use of flange gasket 20 and -is protected from the heat by several layers of insulation 21. An example of the kind of insulation ~sed is aluminum foil backed fibrous aluminum silicate. A ~ath thermocouple is provided w~th a protection tu~e (not ~hown), Gas d~tributor 1 and the motor ~not ~hown) ~re connected to and supported by a superstructure ~not shown) .
- E~ch heatin8 element 17 i8 slidably attached to roof 5 80 that it can move as dual function ~lock 18 expands, 10,971 l~Z45~

still another feature of this invention. Element 17 is inserted in a hole drilled in block 18. Contact between element 17 and block 18 is prevented by spacer 24 and heat baffle 25. Provision for slidable attachment is made to accommodate the thermal expansion of dual function block 18. The particular attachment is conventional and is not shown. When the furnace is brought up to operating temperature and block 18 has expanded element 17 is then fixed in position. When the furnace is cooled down for any reason, element 17 attachment (not shown) to roof 5 i8 loosened 80 that it can ve freely with the contraction of block 18 Elements 17 are usually perpendicular to the roof and bottom of the furnace and parallel to each other.
It is preferred that the material used for distributor 1, the various plstes and other pieces is graphite.
Where any graphite is sbove the level of the melt, however, it is suggested th~t t~e graphite be coated with, e.g., a ceramlc paint, or that other protection i8 provided against oxidation even though seals and a protective atmosphere are utilized or silicon carbide can be substituted for the graphite.
A motor, temperature control, tran~former, and other conventional equipment (all not s~own) are provided to drive distributor l and operate heating elements 17.
Sealing of inlet and outlet ports, piping, and other lo, 97 equipment to protect the integrity of a closed system is also conventional and not shown.

Claims (11)

I CLAIM:

1. A vessel adapted for maintaining metal in a molten state comprising, in combination:
(a) an insulating refractory shell impervious to molten metal;
(b) a lining for a major proportion of that interior surface of said shell, which will be below the surface of the melt, said lining comprising graphite or silicon carbide blocks, which are free to expand in at least one direction in response to the application of heat; and (c) at least one heating means disposed within any of the blocks.

2. Apparatus for refining molten metal comprising, in combination:
(a) the vessel defined in claim 1;
(b) at least one rotating gas distributing means disposed in said vessel; and (c) inlet ant outlet means for molten metal and gases.

3. The apparatus defined in claim 2 having one rotating gas distributing means.

4. The apparatus defined in claim 2 wherein the vessel is closed.

5. The apparatus defined in claim 3 wherein the vessel is closed.

6. The apparatus defined in claim 3 wherein the vessel has a working compartment and an exit compartment, and the working compartment is connected to the exit compartment in such a manner that turbulent melt flowing from the working compartment to the exit compartment will be dampened to an essentially quiescent state.

7. The apparatus defined in claim 4 wherein the heating means is an electric resistance heating element.

8. The apparatus defined in claim 5 wherein the heating means is an electric resistance heating element.

9. The apparatus defined in claim 7 wherein the lining is graphite.

10. The apparatus defined in claim 8 wherein the lining is graphite.

11. The apparatus defined in claim 10 wherein the vessel has a roof and the heating element is slidably attached to the roof in such a manner that it moves on expansion or contraction of the block within which it is disposed.

CA284,080A 1976-08-16 1977-08-04 Apparatus for refining molten metal Expired CA1082456A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US714,669 1976-08-16
US05/714,669 US4040610A (en) 1976-08-16 1976-08-16 Apparatus for refining molten metal
KR7701903A KR810000403B1 (en) 1976-08-16 1977-08-16 Molten Metal Refining Device

Publications (1)

Publication Number Publication Date
CA1082456A true CA1082456A (en) 1980-07-29

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CA284,080A Expired CA1082456A (en) 1976-08-16 1977-08-04 Apparatus for refining molten metal

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US (1) US4040610A (en)
JP (1) JPS5323806A (en)
KR (1) KR810000403B1 (en)
AR (1) AR216773A1 (en)
AT (1) AT364171B (en)
AU (1) AU509438B2 (en)
BE (1) BE857837A (en)
BR (1) BR7705375A (en)
CA (1) CA1082456A (en)
CH (1) CH624478A5 (en)
CS (1) CS207478B1 (en)
DD (1) DD132449A5 (en)
DE (1) DE2736793C2 (en)
ES (2) ES461601A1 (en)
FR (1) FR2362213A1 (en)
GB (1) GB1590063A (en)
GR (1) GR62638B (en)
IE (1) IE45466B1 (en)
IN (1) IN149328B (en)
IT (1) IT1079449B (en)
NL (1) NL188171C (en)
NZ (1) NZ184919A (en)
RO (1) RO75233A (en)
SE (1) SE428500B (en)
YU (1) YU39813B (en)
ZA (1) ZA774575B (en)

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Also Published As

Publication number Publication date
ZA774575B (en) 1978-06-28
SE428500B (en) 1983-07-04
IE45466L (en) 1978-02-16
GR62638B (en) 1979-05-15
AU509438B2 (en) 1980-05-15
YU39813B (en) 1985-04-30
RO75233A (en) 1981-04-30
BR7705375A (en) 1979-03-13
FR2362213A1 (en) 1978-03-17
GB1590063A (en) 1981-05-28
FR2362213B1 (en) 1984-06-22
ES464220A1 (en) 1978-07-01
US4040610A (en) 1977-08-09
AT364171B (en) 1981-09-25
IE45466B1 (en) 1982-09-08
BE857837A (en) 1978-02-16
NL188171C (en) 1992-04-16
CH624478A5 (en) 1981-07-31
NL188171B (en) 1991-11-18
IT1079449B (en) 1985-05-13
ES461601A1 (en) 1978-06-16
JPS5323806A (en) 1978-03-04
NZ184919A (en) 1980-08-26
CS207478B1 (en) 1981-07-31
SE7709192L (en) 1978-02-17
JPS5631849B2 (en) 1981-07-24
AU2792877A (en) 1979-06-21
KR810000403B1 (en) 1981-04-29
AR216773A1 (en) 1980-01-31
IN149328B (en) 1981-10-24
DD132449A5 (en) 1978-09-27
DE2736793C2 (en) 1982-11-11
YU196377A (en) 1982-10-31
ATA588777A (en) 1981-02-15
NL7708989A (en) 1978-02-20
DE2736793A1 (en) 1978-02-23

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1997-07-29 MKEX Expiry